CN107634810B - Satellite energy detection cognitive method and system based on radio environment map - Google Patents

Satellite energy detection cognitive method and system based on radio environment map Download PDF

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CN107634810B
CN107634810B CN201710773826.5A CN201710773826A CN107634810B CN 107634810 B CN107634810 B CN 107634810B CN 201710773826 A CN201710773826 A CN 201710773826A CN 107634810 B CN107634810 B CN 107634810B
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张建军
薛明
张蕾
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China Academy of Space Technology CAST
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Abstract

A satellite energy detection cognitive method and system based on a radio environment map are as follows: (1) analyzing interference caused by a Fixed Service (FS) link to a Fixed Satellite Service (FSS) link in a satellite/terrestrial communication scenario; (2) according to a spectrum energy detection method, cognitive equipment obtains decision statistic distribution of received interference signal energy, and interference information of the cognitive equipment is obtained through the fact that the decision statistic is larger than a certain predetermined threshold probability; (3) in a certain interference area with GPS cognitive equipment, converting a geodetic coordinate system of the cognitive equipment into a preset navigation coordinate system to obtain position information (x, y) of the cognitive equipment; (4) and the cognitive equipment transmits the interference information and the position information to a data center through an undisturbed control channel to finish the accurate drawing of the radio environment map. The invention reuses the idle frequency spectrum resources in the airspace, the frequency domain and the time domain, and improves the utilization rate of the existing quite tense radio frequency spectrum resources.

Description

Satellite energy detection cognitive method and system based on radio environment map
Technical Field
The invention relates to a satellite energy detection cognitive method and system based on a radio environment map, which allows a satellite link to develop unused spectrum resources of a ground link in a more efficient mode and meets the challenge of spectrum shortage in a satellite wireless communication system.
Background
With the development of wireless communication technology, the number of wireless users is rapidly increased, the spectrum demand is rapidly increased, and the problem of spectrum scarcity is increasingly highlighted. Meanwhile, a large number of measurement results show that the utilization rate of the allocated frequency band is not high, and it can be seen that the shortage of the frequency spectrum is not the shortage of the frequency spectrum resource, so how to use the radio frequency spectrum resource more efficiently is an important problem to be solved urgently. The cognitive radio technology is recognized as a technology for solving the spectrum scarcity problem, and it can be adapted to the environment more conveniently and easily, and can find and use radio resources in a more efficient manner, and in the last years, a great deal of research has been conducted on applying the cognitive radio technology to a ground system, and also, using the cognitive radio technology on a satellite system, using the advantages of satellite communication, the interest of providing a more reliable cognitive level is increasing.
In a satellite/terrestrial scene, the cognitive radio perception technology based on a radio environment map is used, and the main problems exist:
(1) there are specific requirements for satellite communications that need to be considered, and one of the important challenges facing the application of cognitive technology to satellite systems is the satellite environment, i.e., the inherent nature of satellite communications. The satellite communication has the characteristics of large-range area coverage and limited ground receiving power caused by long communication distance, and how to consider the application of the cognitive technology under the characteristics of a satellite scene is a problem.
(2) Because microwave frequency ranges are very concentrated, Fixed Satellite Services (FSS) and Fixed Services (FS) often share links, the considered cognitive radio technology needs to analyze interference caused by the FS links to the FSS links, reuse spectrum resources which are not used by the FS, and ensure that mutual interference is under a certain threshold value and distinguish which frequencies are used and which frequencies are not used by the FS;
(3) in terrestrial systems, Interference mapping (Interference Cartography) and Radio Environment Mapping (REM) techniques are used as a method to provide a spatial description of the Interference, achieving a wider experience of the Environment. The problem of spectrum characteristics cannot be solved by information about the existing spectrum utilization obtained from a database or information only depending on one cognitive device, and the problem is only that the information is limited to the position of a sensing node, so that how to collect information by using multiple sensing nodes in a coordinated manner is a problem to be considered;
(4) the current radio environment map lacks a real-time spectrum sensing function under various combinations of frequency, geography and time, so that the efficiency of spectrum allocation and sharing is not high, the automatic spectrum management function cannot be realized, and the efficiency of a total cognitive system is reduced.
Disclosure of Invention
The technical problem solved by the invention is as follows: the method and the system for detecting and recognizing the satellite energy based on the radio environment map are provided, the advantage of wide-range coverage of satellite communication is utilized, a radio frequency spectrum sensing method is developed by adopting a radio environment map technology, and the problem of spectrum utilization is solved.
The technical solution of the invention is as follows: the cognitive method of the energy detector based on the radio environment map comprises the following steps:
(1) in a satellite/terrestrial scene, judging whether an FS link causes interference on an FSS link, if so, performing the step (2), otherwise, judging that the FS link and the FSS link are independent links;
(2) according to a spectrum energy detection method, within a certain time T and a link communication bandwidth B, obtaining the energy distribution of interference signals of different frequency bands of an FS link to an FSS link received by cognitive equipment C, comparing the energy of the interference signals of the different frequency bands with a preset energy detection threshold value, obtaining the ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands, and obtaining the ratio of the number of the interference signals of the frequency bands which is less than the preset energy detection threshold value to the number of the interference signals of all the frequency bands, so as to obtain the interference information of the cognitive equipment C;
(3) the cognitive device C provided with the GPS is deployed in a certain interference area, and coordinates of the cognitive device C obtained by the GPS under a geodetic coordinate system are converted into coordinates under a navigation coordinate system, so that position information (x, y) of each cognitive device under the navigation coordinate system is obtained;
(4) and the cognitive device C transmits the interference information of the device C and the position information of each cognitive device in the navigation coordinate system to a data center through a channel which is not interfered by an FS link in a communication link between the satellite A and the cognitive device C, so that the radio environment map is accurately drawn.
In a satellite/terrestrial scene, judging whether an FS link causes interference on an FSS link or not, and comprising the following steps:
establishing an interference evaluation model, namely determining different interference combinations between the FS link and the FSS link according to the positions of the terminal antennas of the FS link and the FSS link, the directions and the elevation angles of the antennas, and selecting a specific mode, namely only considering the parallel direction and the orthogonal direction, because the pointing angle formed by the connection line of the antenna of the terminal B in the FS link and the cognitive user C in the FSS link and the pointing angle formed by the connection line of the antenna of the GEO satellite A and the cognitive user C in the FSS link and the horizontal plane are arbitrary. Since the interference is substantially negligible in the orthogonal case, the parallel direction is chosen for analysis.
In the step (2), the spectrum energy is detectedThe measured integration time is T, the link communication bandwidth is B, the signal-to-noise ratio is SNR, and the product of the time and the bandwidth is NobsThe preset energy detection threshold is xi, and the cognitive device C detects the probability of the interference of the FS link to the FSS link
Figure GDA0002661058670000031
The ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands, and the probability of no interference detection (false alarm rate)
Figure GDA0002661058670000032
That is, the ratio of the number of the interference signals in these frequency bands smaller than the preset energy detection threshold to the number of the interference signals in all the frequency bands is represented as:
Figure GDA0002661058670000033
Figure GDA0002661058670000034
wherein
Figure GDA0002661058670000035
Is the normalized gamma function:
Figure GDA0002661058670000036
wherein a is Nobs,
Figure GDA0002661058670000037
Figure GDA0002661058670000038
The cognitive device C provided with the GPS is deployed in a certain interference area, and coordinates of the cognitive device C obtained by the GPS under a geodetic coordinate system are converted into coordinates under a navigation coordinate system, so that position information (x, y) of each cognitive device under the navigation coordinate system is obtained;
Figure GDA0002661058670000041
wherein R1-40075360 m denotes the equatorial length, R2-39940670 m denotes the warp length; b is the geodetic latitude (B)0And B1Respectively, different longitude values), L is the geodetic longitude (L)1And L0Different latitude values respectively), x is an east-west azimuth coordinate value, and y is a north-south azimuth coordinate value.
The navigation coordinate system is defined, the origin is the earth's centroid, the coordinate axes are directed fixed relative to the stars, three-dimensional, the X-axis is directed from the earth's centroid to the vernalia point, the XY-plane is coincident with the earth's equatorial plane, the Z-axis is perpendicular to the XY-plane and directed in the direction of the north pole, and the Y-axis is oriented to form a right-hand coordinate system.
The radio environment map displays time domain, frequency domain and energy domain information of the radio environment on the map based on a geographic information system.
The radio environment map comprises the spectrum distribution situation of each position in the interference area.
Cognitive system of energy detector based on radio environment map, include: the device comprises a judging module, an interference information obtaining module, a position information obtaining module and a transmission drawing module;
the judging module is used for judging whether the FS link interferes the FSS link or not in a satellite/terrestrial scene, if so, the interference information obtaining module obtains the energy distribution of interference signals of different frequency bands of the FSS link received by the cognitive device C within a certain time T and a link communication bandwidth B according to a frequency spectrum energy detection method, compares the energy of the interference signals of the different frequency bands with a preset energy detection threshold value, obtains the ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands, and obtains the ratio of the number of the interference signals of the frequency bands which is less than the preset energy detection threshold value to the number of the interference signals of all the frequency bands, so that the interference information of the cognitive device C is obtained; otherwise, judging the FS link and the FSS link as independent links;
the position information acquisition module is used for deploying the cognitive equipment C provided with the GPS in a certain interference area, and converting the coordinates of the cognitive equipment C obtained by the GPS in a geodetic coordinate system into the coordinates in a navigation coordinate system to obtain the position information (x, y) of each cognitive equipment in the navigation coordinate system;
and the transmission drawing module is used for controlling the cognitive equipment C to transmit the interference information of the equipment C and the position information of each cognitive equipment in the navigation coordinate system to the data center through a channel which is not interfered by an FS link in a communication link between the satellite A and the cognitive equipment C, so that the radio environment map is accurately drawn.
In a satellite/terrestrial scene, judging whether an FS link causes interference on an FSS link or not, and comprising the following steps: and establishing an interference evaluation model, namely determining different interference combinations between the FS link and the FSS link according to the positions of the communication link terminal antennas in the FS link and the FSS link, and the direction and the elevation angle of the antennas, wherein the pointing angle formed by the connection line of the antenna of the terminal B in the FS link and the cognitive user C in the FSS link and the horizontal plane and the pointing angle formed by the connection line of the antenna of the GEO satellite A and the cognitive user C and the horizontal plane are arbitrary.
In the interference information acquisition module, the integral time of the spectrum energy detection is T, the link communication bandwidth is B, the signal-to-noise ratio is SNR, and the time bandwidth product is NobsThe preset energy detection threshold is xi, and the cognitive device C detects the probability of the interference of the FS link to the FSS link
Figure GDA0002661058670000051
The ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands, and the probability of no interference detection (false alarm rate)
Figure GDA0002661058670000052
That is, the number of interference signals in these frequency bands smaller than the preset energy detection threshold value accounts forThe ratio of the number of the frequency band interference signals is expressed as:
Figure GDA0002661058670000053
Figure GDA0002661058670000054
wherein
Figure GDA0002661058670000055
Is the normalized gamma function:
Figure GDA0002661058670000056
wherein a is Nobs,
Figure GDA0002661058670000057
Figure GDA0002661058670000058
The cognitive device C provided with the GPS is deployed in a certain interference area, and coordinates of the cognitive device C obtained by the GPS under a geodetic coordinate system are converted into coordinates under a navigation coordinate system, so that position information (x, y) of each cognitive device under the navigation coordinate system is obtained;
Figure GDA0002661058670000061
wherein R1-40075360 m denotes the equatorial length, R2-39940670 m denotes the warp length; b is0And B1Respectively, are different longitude values, L1And L0Respectively different latitude values, wherein x is an east-west azimuth coordinate value, and y is a north-south azimuth coordinate value;
the navigation coordinate system is defined, the origin is the earth's centroid, the coordinate axes are directed fixed relative to the stars, three-dimensional, the X-axis is directed from the earth's centroid to the vernalia point, the XY-plane is coincident with the earth's equatorial plane, the Z-axis is perpendicular to the XY-plane and directed in the direction of the north pole, and the Y-axis is oriented to form a right-hand coordinate system.
Compared with the prior art, the invention has the advantages that:
(1) by using an interleaving radio technology, the sensing node uses an energy detector to complete the detection of interference signals, and more reliable environment knowledge is provided;
(2) a sensing node is provided with a GPS global positioning navigation receiver, and the sensed interference information carries the position information of an interference point, so that the spatial description of the interference can be obtained;
(3) by utilizing the advantages of satellite communication, compared with the sensing of a pure ground system, a large amount of interference conditions can be transmitted to a ground data center, and the real-time performance, the universality and the cooperation performance of sensing information acquisition are ensured to the greatest extent;
(4) the map can be directly updated through the measurement of the distributed cognitive wireless equipment, and the drawn frequency spectrum map is displayed and updated in real time in a time domain, a frequency domain and a space domain three-dimensional image, so that the map can be more vividly and intuitively used by operators;
(5) the same cooperative wireless cognitive device can access a map, can also be accessed by a newly added wireless cognitive device, and integrates the past information into the existing measurement;
(6) the wireless cognitive device with low complexity and low cost, which is not provided with a specific technology for self-performing external environment detection, can access the map;
(7) a frequency spectrum sensing technology based on a wireless environment map introduces a land-dominated interference strategy and a wireless environment map technology as a method for providing space-time interference information, which is particularly important for wide-range coverage application of satellite communication, and effectively improves the efficiency of a cognitive satellite system.
Drawings
FIG. 1 is a diagram of a satellite/terrestrial communications scenario;
FIG. 2 is a flow chart of a method for detecting satellite energy based on a radio environment map;
fig. 3(a) is an interference estimation model diagram when the azimuth is 0, (b) is an interference estimation model diagram when the azimuth is 90, (c) is an interference estimation model diagram when the azimuth is 180, and (d) is an interference estimation model diagram when the azimuth is 270;
FIG. 4 is a graph of interference levels at (a) first spatial midpoint and (b) second spatial midpoint;
FIG. 5 is a block diagram of an energy detection method;
FIG. 6 is an exemplary diagram of a scattered binary test.
Detailed Description
The invention is described in detail below with reference to the figures and specific embodiments.
The invention relates to a satellite energy detection cognitive method based on a radio environment map, which comprises the following steps: (1) analyzing interference caused by a Fixed Service (FS) link to a Fixed Satellite Service (FSS) link in a satellite/terrestrial communication scenario; (2) according to a spectrum energy detection method, cognitive equipment obtains decision statistic distribution of received interference signal energy, and interference information of the cognitive equipment is obtained through the fact that the decision statistic is larger than a certain predetermined threshold probability in a certain range; (3) in a certain interference area with GPS cognitive equipment, converting a geodetic coordinate system of the cognitive equipment into a preset navigation coordinate system to obtain position information (x, y) of each cognitive equipment; (4) and the cognitive equipment transmits the interference information and the position information to a data center through a special undisturbed control channel to finish the accurate drawing of the radio environment map. The invention reuses the idle frequency spectrum resources in the airspace, the frequency domain and the time domain, and improves the utilization rate of the existing quite tense radio frequency spectrum resources.
The invention relates to a satellite energy detection cognitive method based on a radio environment map, which comprises the following steps:
(1) analyzing interference caused by FS link to FSS link in satellite/terrestrial scene
(2) According to a spectrum energy detection method, cognitive equipment obtains decision statistic distribution of received interference signal energy, and in a certain time T and a certain bandwidth B, whether interference signals exist or not can be determined through the fact that the decision statistic is larger than a certain predetermined threshold probability, and interference information of the cognitive equipment is obtained;
(3) cognitive equipment provided with a GPS is deployed in a certain interference area, and a geodetic coordinate system of the cognitive equipment is converted into a preset navigation coordinate system to obtain position information (x, y) of each cognitive equipment;
(4) and the cognitive equipment transmits the interference information and the position information to a data center through a special undisturbed control channel to finish the accurate drawing of the radio environment map.
Defining a satellite/terrestrial scene as shown in fig. 1, Main lobe direction represents a Main lobe direction of a satellite antenna, Interference Path represents an Interference Path, and communication service operates in 17.7 and 19.7GHz frequency bands. Wherein A is a GEO satellite, B and C are two fixed points (communication devices) in the same geographic coverage area respectively, A, B, C are communication link terminals, both are provided with antennas for receiving and transmitting information, and A and C can communicate with each other. And an allocated FS link exists between B and C, and is an authorized user. The GEO satellite can transmit data with a user C through an FSS link, wherein the C is a cognitive user, namely cognitive equipment, a GPS is installed on the C, and the number of the cognitive equipment can be one or more. And reusing the spectrum resources which are not used by the FS through cognitive means, and ensuring that the mutual interference between the FS and the FSS is lower than a certain threshold value.
As shown in fig. 2, the method comprises the following specific steps:
step 1: the interference caused by the FS link to the FSs link in a satellite/terrestrial scenario is analyzed.
As shown in fig. 3(a), (b), (c), and (d), there are several different interference combinations depending on the location, azimuth, direction, and elevation of the FS and FSs antennas. Since the pointing angles of the FS transmitter and the FSs ground are arbitrary, the analysis is limited to a set of mutual directions, parallel and orthogonal. Case2 and Case4 are essentially identical and are easily understood because they are orthogonal cases, and this interference is essentially negligible, and due to space constraints, only Case3 was chosen for analysis.
In fig. 3, L denotes the side length of the sensing region, x denotes the abscissa of the device C within the sensing region; y denotes the ordinate of the device C within the perception area, azimuthFS referring to the orientation angle between the device B and the device C.
In fig. 4, the interference level at a point in space is represented by the intensity of different gray levels. The black area of the right b-diagram represents Ir>ImaxIn the case of (channel occupancy), white area indicates Ir<ImaxSituation (channel free). I ismaxRepresenting the maximum tolerated interference level. We can observe that in fig. 3, the dominant position of the FS transmitter occupies the entire form of interference, except for Ir>ImaxMainly determines the direction and width of the FS which is mainly unknown. As shown below, we consider Imax-141dB/MHz, as specified by ITU2012 "Radio Regulations". And B is set at the position of an origin, a horizontal axis X and a vertical axis Y are directions parallel to and perpendicular to the FS link respectively, and horizontal and vertical coordinate values are coordinate values of the position of C in the coordinate system respectively.
As shown in (a) and (b) of fig. 4, the Interference Power represents Interference energy, the Interference Binary Hard Test represents a Binary grayscale Test of Interference, and X represents a distance between two adjacent sides of the sensing region. Y denotes a distance of the other of the adjacent two sides representing the sensing region.
In the reference scenario, since there is no a priori knowledge of the FS interference, a way to black-box detect all types of interference signals is taken. In the black box detector, the energy detector is chosen because it has the advantage of low design complexity, but on the other hand has the disadvantage of not being detectable with a low power signal. Furthermore, noise from the receiver may trigger detection even if no interference exists due to the setting of the threshold by the hardware device.
Step 2: according to a spectrum energy detection method, cognitive equipment obtains decision statistic distribution of received interference signal energy, and in a certain time T and a certain bandwidth B, whether interference signals exist or not can be determined through the fact that the decision statistic is larger than a certain predetermined threshold probability, and interference information of the cognitive equipment is obtained.
As shown in fig. 5, RX signal represents signals transmitted from a satellite, BPF refers to a band pass filter,b denotes the bandwidth, (-) 2 denotes squaring,
Figure GDA0002661058670000091
it is shown that the integration is performed,
Figure GDA0002661058670000092
the representation is compared with a threshold value, and xi represents the threshold value;
as shown in fig. 5, first, the signal at the antenna input end at point C is filtered by a band-pass filter, and the bandwidth is B, and under the assumption of AWGN white gaussian noise channel, the received signal r (t) is represented as follows:
Figure GDA0002661058670000093
where s (t) is the signal due to FS interference, h is the amplitude gain of the channel, and v (t) is the power spectral density N0The AWGN noise signal of (a). The noise power is expressed as follows:
σ2=E{v(t)2}=N0B (2)
considering complex noise, the real and imaginary parts of the v (t) signal follow a chi-squared distribution
Figure GDA0002661058670000094
According to the assumption H0(single sense) or H1(single presence), noise or noise plus the transmitted signal, respectively, into the antenna input receiver. The detection test statistic Δ represents the energy of the measured received signal over a time interval T, and the statistic Δ is then compared with a suitably chosen threshold ξ as a binary test:
Figure GDA0002661058670000101
for simplification, it is assumed that the observation interval start time t is 0.
The performance of the energy detector can be determined with the probability of correct detection
Figure GDA0002661058670000102
And probability of false alarm
Figure GDA0002661058670000103
Estimate the probability of detecting the transmitted signal, respectively, at the time of the main transmitted signal
Figure GDA0002661058670000104
Probability of detecting a transmitted signal in the absence of a transmitted signal
Figure GDA0002661058670000105
Figure GDA0002661058670000106
Represents H1Is estimated. In the scenario considered, low
Figure GDA0002661058670000107
Consistent with the high probability of not detecting primary user transmission signals, and also receiving undesirable interference. On the other hand, high
Figure GDA0002661058670000108
Meaning that the probability of missing a transmission opportunity is high and also lower spectral reuse efficiency. For energy detectors, evaluation
Figure GDA0002661058670000109
And
Figure GDA00026610586700001010
the equation is in the form:
Figure GDA00026610586700001011
Figure GDA00026610586700001012
wherein the time bandwidth product NobsTB, further can be represented as:
Figure GDA00026610586700001013
Figure GDA00026610586700001014
wherein
Figure GDA00026610586700001015
Is the normalized gamma function:
Figure GDA00026610586700001016
Figure GDA00026610586700001017
and step 3: the cognitive device provided with the GPS is deployed in a certain interference area, the geodetic coordinate system of the cognitive device is converted into a preset navigation coordinate system, and the position information (x, y) of each cognitive device is obtained.
The cognitive device is provided with a GPS positioning chip, and the geodetic coordinates of a certain cognitive device A are (B0, L0), and the geodetic coordinates of another cognitive device B are (B1, L1). And selecting A as the origin of the navigation coordinate system, and obtaining the coordinates (x, y) of the point B in the navigation coordinate system with the point A as the origin according to a formula (8).
Figure GDA00026610586700001018
Wherein R1-40075360 m denotes the equatorial length, R2-39940670 m denotes the warp length; b is the geodetic latitude (B)0And B1Respectively, different longitude values), L is the geodetic longitude (L)1And L0Respectively different latitude values), x is an east-west orientation coordinate value, and y is a north-south orientation coordinate value。
And 4, step 4: the cognitive device transmits the interference information and the position information to a data center through a special undisturbed control channel to finish the accurate drawing of a radio environment map;
the invention relates to a cognitive system of an energy detector based on a radio environment map, which comprises: the device comprises a judging module, an interference information obtaining module, a position information obtaining module and a transmission drawing module;
the judging module is used for judging whether the FS link interferes the FSS link or not in a satellite/terrestrial scene, if so, the interference information obtaining module obtains the energy distribution of interference signals of different frequency bands of the FSS link received by the cognitive device C within a certain time T and a link communication bandwidth B according to a frequency spectrum energy detection method, compares the energy of the interference signals of the different frequency bands with a preset energy detection threshold value, obtains the ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands, and obtains the ratio of the number of the interference signals of the frequency bands which is less than the preset energy detection threshold value to the number of the interference signals of all the frequency bands, so that the interference information of the cognitive device C is obtained; otherwise, judging the FS link and the FSS link as independent links;
the position information acquisition module is used for deploying the cognitive equipment C provided with the GPS in a certain interference area, and converting the coordinates of the cognitive equipment C obtained by the GPS in a geodetic coordinate system into the coordinates in a navigation coordinate system to obtain the position information (x, y) of each cognitive equipment in the navigation coordinate system;
and the transmission drawing module is used for controlling the cognitive equipment C to transmit the interference information of the equipment C and the position information of each cognitive equipment in the navigation coordinate system to the data center through a channel which is not interfered by an FS link in a communication link between the satellite A and the cognitive equipment C, so that the radio environment map is accurately drawn.
In a satellite/terrestrial scene, judging whether an FS link causes interference on an FSS link or not, and comprising the following steps: and establishing an interference evaluation model, namely determining different interference combinations between the FS link and the FSS link according to the positions of the communication link terminal antennas in the FS link and the FSS link, and the direction and the elevation angle of the antennas, wherein the pointing angle formed by the connection line of the antenna of the terminal B in the FS link and the cognitive user C in the FSS link and the horizontal plane and the pointing angle formed by the connection line of the antenna of the GEO satellite A and the cognitive user C and the horizontal plane are arbitrary.
In the interference information acquisition module, the integral time of the spectrum energy detection is T, the link communication bandwidth is B, the signal-to-noise ratio is SNR, and the time bandwidth product is NobsThe preset energy detection threshold is xi, and the cognitive device C detects the probability of the interference of the FS link to the FSS link
Figure GDA0002661058670000121
The ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands, and the probability of no interference detection (false alarm rate)
Figure GDA0002661058670000122
That is, the ratio of the number of the interference signals in these frequency bands smaller than the preset energy detection threshold to the number of the interference signals in all the frequency bands is represented as:
Figure GDA0002661058670000123
Figure GDA0002661058670000124
wherein
Figure GDA0002661058670000125
Is the normalized gamma function:
Figure GDA0002661058670000126
wherein a is Nobs,
Figure GDA0002661058670000127
Figure GDA0002661058670000128
The cognitive device C provided with the GPS is deployed in a certain interference area, and coordinates of the cognitive device C obtained by the GPS under a geodetic coordinate system are converted into coordinates under a navigation coordinate system, so that position information (x, y) of each cognitive device under the navigation coordinate system is obtained;
Figure GDA0002661058670000129
wherein R1-40075360 m denotes the equatorial length, R2-39940670 m denotes the warp length; b is0And B1Respectively, are different longitude values, L1And L0Respectively different latitude values, wherein x is an east-west azimuth coordinate value, and y is a north-south azimuth coordinate value;
the navigation coordinate system is defined, the origin is the earth's centroid, the coordinate axes are directed fixed relative to the stars, three-dimensional, the X-axis is directed from the earth's centroid to the vernalia point, the XY-plane is coincident with the earth's equatorial plane, the Z-axis is perpendicular to the XY-plane and directed in the direction of the north pole, and the Y-axis is oriented to form a right-hand coordinate system.
The cognitive wireless device transmits its own binary measure of the presence of interference to the designated data fusion center via a dedicated control channel (extra band reserved for FSS) that is not subject to interference. Furthermore, a cognitive wireless device is a device that has a location estimate installed (e.g., GPS or other similar device) so that the fusion center can map the measurements it collects spatially accurately. After the data fusion center collects the data of the wireless cognitive device, the fusion center can elaborate a Radio Environment Map (REM), which gives a spatial description of the interference, as shown in fig. 6, where X represents the distance between two adjacent sides of the sensing area. Y denotes a distance of the other of the adjacent two sides representing the sensing region.
The frequency spectrum map is stored according to the sensed data, is displayed by icons in three dimensions of time domain, frequency domain and airspace in combination with the existing geographic and topographic database information, and can be updated in real time. The output of advanced maps is in 2 forms, 2D and 3D. As shown in fig. 6, the map area is composed of a series of grids (minimum resolution) corresponding to the geographical location of the test area, the center of the map is the location of the test point, and the gray levels of the different test areas represent the different radio frequency powers received at the locations.

Claims (8)

1. The cognitive method of the energy detector based on the radio environment map is characterized by comprising the following steps of:
(1) in a satellite/terrestrial scene, judging whether an FS link causes interference on an FSS link, if so, performing the step (2), otherwise, judging that the FS link and the FSS link are independent links;
(2) according to a spectrum energy detection method, within a certain time T and a link communication bandwidth B, obtaining the energy distribution of interference signals of different frequency bands of an FS link to an FSS link received by cognitive equipment C, comparing the energy of the interference signals of the different frequency bands with a preset energy detection threshold value, obtaining the ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands, and obtaining the ratio of the number of the interference signals of the frequency bands which is less than the preset energy detection threshold value to the number of the interference signals of all the frequency bands, so as to obtain the interference information of the cognitive equipment C;
in the step (2), the integration time of the spectrum energy detection is T, the link communication bandwidth is B, the signal-to-noise ratio is SNR, and the time bandwidth product is NobsThe preset energy detection threshold is xi, and the cognitive device C detects the probability of the interference of the FS link to the FSS link
Figure FDA0002710493940000011
The ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands and the probability of detecting the transmission signal when the transmission signal is not transmitted
Figure FDA0002710493940000012
That is, the ratio of the number of the interference signals in these frequency bands smaller than the preset energy detection threshold to the number of the interference signals in all frequency bands is expressed as:
Figure FDA0002710493940000013
Figure FDA0002710493940000014
wherein
Figure FDA0002710493940000015
Is the normalized gamma function:
Figure FDA0002710493940000016
wherein a is Nobs,
Figure FDA0002710493940000017
Figure FDA0002710493940000018
(3) The cognitive device C provided with the GPS is deployed in a certain interference area, and coordinates of the cognitive device C obtained by the GPS under a geodetic coordinate system are converted into coordinates under a navigation coordinate system, so that position information (x, y) of each cognitive device under the navigation coordinate system is obtained;
(4) and the cognitive device C transmits the interference information of the device C and the position information of each cognitive device in the navigation coordinate system to a data center through a channel which is not interfered by an FS link in a communication link between the satellite A and the cognitive device C, so that the radio environment map is accurately drawn.
2. The cognitive method of an energy detector based on a radio environment map as claimed in claim 1, wherein: in a satellite/terrestrial scene, judging whether an FS link causes interference on an FSS link or not, and comprising the following steps: and establishing an interference evaluation model, namely determining different interference combinations between the FS link and the FSS link according to the positions of the communication link terminal antennas in the FS link and the FSS link, and the direction and the elevation angle of the antennas, wherein the pointing angle formed by the antenna of the terminal B in the FS link and the connection line of the cognitive user C in the FSS link and the horizontal plane and the pointing angle formed by the connection line of the antenna of the satellite A and the cognitive user C and the horizontal plane are arbitrary.
3. The cognitive method of an energy detector based on a radio environment map as claimed in claim 1, wherein: the cognitive device C provided with the GPS is deployed in a certain interference area, and coordinates of the cognitive device C obtained by the GPS under a geodetic coordinate system are converted into coordinates under a navigation coordinate system, so that position information (x, y) of each cognitive device under the navigation coordinate system is obtained;
Figure FDA0002710493940000021
wherein R1-40075360 m denotes the equatorial length, R2-39940670 m denotes the warp length; b is0And B1Respectively, are different longitude values, L1And L0Respectively different latitude values, wherein x is an east-west azimuth coordinate value, and y is a north-south azimuth coordinate value;
the navigation coordinate system is defined, the origin is the earth's centroid, the coordinate axes are directed fixed relative to the stars, three-dimensional, the X-axis is directed from the earth's centroid to the vernalia point, the XY-plane is coincident with the earth's equatorial plane, the Z-axis is perpendicular to the XY-plane and directed in the direction of the north pole, and the Y-axis is oriented to form a right-hand coordinate system.
4. The cognitive method of an energy detector based on a radio environment map as claimed in claim 1, wherein: the radio environment map displays time domain, frequency domain and energy domain information of the radio environment on the map based on a geographic information system.
5. The cognitive method of an energy detector based on a radio environment map as claimed in claim 1, wherein: the radio environment map comprises the spectrum distribution situation of each position in the interference area.
6. Cognitive system of energy detector based on radio environment map, characterized by that includes: the device comprises a judging module, an interference information obtaining module, a position information obtaining module and a transmission drawing module;
the judging module is used for judging whether the FS link interferes the FSS link or not in a satellite/terrestrial scene, if so, the interference information obtaining module obtains the energy distribution of interference signals of different frequency bands of the FSS link received by the cognitive device C within a certain time T and a link communication bandwidth B according to a frequency spectrum energy detection method, compares the energy of the interference signals of the different frequency bands with a preset energy detection threshold value, obtains the ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands, and obtains the ratio of the number of the interference signals of the frequency bands which is less than the preset energy detection threshold value to the number of the interference signals of all the frequency bands, so that the interference information of the cognitive device C is obtained; otherwise, judging the FS link and the FSS link as independent links;
in the interference information acquisition module, the integral time of the spectrum energy detection is T, the link communication bandwidth is B, the signal-to-noise ratio is SNR, and the time bandwidth product is NobsThe preset energy detection threshold is xi, and the cognitive device C detects the probability of the interference of the FS link to the FSS link
Figure FDA0002710493940000031
The ratio of the number of the interference signals of the frequency bands which is more than or equal to the preset energy detection threshold value to the number of the interference signals of all the frequency bands and the probability of detecting the transmission signal when the transmission signal is not transmitted
Figure FDA0002710493940000032
That is, the ratio of the number of the interference signals in these frequency bands smaller than the preset energy detection threshold to the number of the interference signals in all frequency bands is expressed as:
Figure FDA0002710493940000033
Figure FDA0002710493940000034
wherein
Figure FDA0002710493940000035
Is the normalized gamma function:
Figure FDA0002710493940000036
wherein a is Nobs,
Figure FDA0002710493940000037
Figure FDA0002710493940000038
The position information acquisition module is used for deploying the cognitive equipment C provided with the GPS in a certain interference area, and converting the coordinates of the cognitive equipment C obtained by the GPS in a geodetic coordinate system into the coordinates in a navigation coordinate system to obtain the position information (x, y) of each cognitive equipment in the navigation coordinate system;
and the transmission drawing module is used for controlling the cognitive equipment C to transmit the interference information of the equipment C and the position information of each cognitive equipment in the navigation coordinate system to the data center through a channel which is not interfered by an FS link in a communication link between the satellite A and the cognitive equipment C, so that the radio environment map is accurately drawn.
7. The cognitive system of energy probes based on radio environment map according to claim 6, characterized by: in a satellite/terrestrial scene, judging whether an FS link causes interference on an FSS link or not, and comprising the following steps: and establishing an interference evaluation model, namely determining different interference combinations between the FS link and the FSS link according to the positions of the communication link terminal antennas in the FS link and the FSS link, and the direction and the elevation angle of the antennas, wherein the pointing angle formed by the antenna of the terminal B in the FS link and the connection line of the cognitive user C in the FSS link and the horizontal plane and the pointing angle formed by the connection line of the antenna of the satellite A and the cognitive user C and the horizontal plane are arbitrary.
8. The cognitive system of energy probes based on radio environment map according to claim 6, characterized by: the cognitive device C provided with the GPS is deployed in a certain interference area, and coordinates of the cognitive device C obtained by the GPS under a geodetic coordinate system are converted into coordinates under a navigation coordinate system, so that position information (x, y) of each cognitive device under the navigation coordinate system is obtained;
Figure FDA0002710493940000041
wherein R1-40075360 m denotes the equatorial length, R2-39940670 m denotes the warp length; b is0And B1Respectively, are different longitude values, L1And L0Respectively different latitude values, wherein x is an east-west azimuth coordinate value, and y is a north-south azimuth coordinate value;
the navigation coordinate system is defined, the origin is the earth's centroid, the coordinate axes are directed fixed relative to the stars, three-dimensional, the X-axis is directed from the earth's centroid to the vernalia point, the XY-plane is coincident with the earth's equatorial plane, the Z-axis is perpendicular to the XY-plane and directed in the direction of the north pole, and the Y-axis is oriented to form a right-hand coordinate system.
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